Structural analysis of KufaSat using ANSYS program

• Autorzy: Al-Maliky Firas T. , AlBermani Mohamed J.

Identyfikatory

DOI

10.2478/arsa-2018-0003

• Języki publikacji: EN

Abstrakty

EN

The current work focuses on vibration and modal analysis of KufaSat structure using ANSYS 16 program. Three types of Aluminum alloys (5052-H32, 6061-T6 and 7075-T6) were selected for investigation of the structure under design loads. Finite element analysis (FEA) in design static load of 51 g was performed. The natural frequencies for five modes were estimated using modal analysis. In order to ensure that KufaSat could withstand with various conditions during launch, the Margin of safety was calculated. The results of deformation and Von Mises stress for linear buckling analysis were also performed. The comparison of data was done to select the optimum material for KufaSat structures.

Słowa kluczowe

EN

CubeSat; modal analysis; structure analysis; natural frequency; FEA

• Wydawca: Centrum Badań Kosmicznych PAN ; De Gruyter
• Czasopismo: Artificial Satellites : Journal of Planetary Geodesy
• Rocznik: 2018
• Tom: Vol. 53, No. 1
• Strony: 29--35
• Opis fizyczny: Bibliogr. 13 poz., rys., tab.

Twórcy

autor

Al-Maliky Firas T.

• Alkafeel University College/Department of Computer Engineering Techniques, Najaf, Iraq

autor

AlBermani Mohamed J.

• Alkafeel University College/Department of Computer Engineering Techniques, Najaf, Iraq

Bibliografia

• [1] Mohammed Chessab Mahdi, “ORBIT DESIGN AND SIMULATION FOR KUFASAT NANOSATELLITE”, ARTIFICIAL SATELLITES, Vol. 50, No. 4, 2015.
• [2] Mohammed Chessab Mahdi1 , Mohammed Jaafar AL-Bermani2 , “LQR Controller for Kufasat”, Technical Institute of Kufa Computer Center1 , University of Kufa-College of Science Department of physics2 , JOURNAL OF KUFA - PHYSICS, Vol.6/ No.1, 2014.
• [3] H.R.Chiranjeeve, K.Kalaichelvan and A.Rajadurai, “Design and Vibration Analysis of a 2U-Cubsat Structure Using AA-6061 for AUNSAT - II”, IOSR Journal of Mechanical and Civil Engineering, 2014.
• [4] Asif Israr, “Vibration and Modal Analysis of Low Earth Orbit Satellite”, Hindawi Publishing Corporation, Shock and Vibration, 2014.
• [5] Hyun-Ung Oh, Su-Hyeon Jeon and Seong-Cheol Kwon,“Structural Design and Analysis of 1U Standardized STEP Cube Lab for On-Orbit Verification of Fundamental Space Technologies”, International Journal of Materials, Mechanics and Manufacturing, 2014.
• [6] VALERITY SHEPENKOV, “Vibration Modal Analysis of a Deployable Boom Integrated to a CubeSat”, School of Engineering Sciences, Department of Mechanics, KTH Royal Institute of Technology, 2013.
• [7] Michael Bauccio, “ASM Metals Reference Book”, Ed. ASM International, Materials Park, OH, Third edition, 1993.
• [8] Howard E. Boyer and Timothy L. Gall, “Metals Handbook”, Eds., American Society for Metals, Materials Park, OH, 1985.
• [9] John M. (Tim) Holt, “Structural Alloys Handbook”, Technical Ed; C. Y. Ho, Ed., CINDAS/Purdue University, West Lafayette, IN, 1996.
• [10] Robert C. Baumann, “GENERAL ENVIRONMENTAL VERIFICATION SPECIFICATION FOR STS & ELV” ,NASA GODDARD SPACE FLIGHT CENTER, 1996.
• [11] Wisam A. Hussain, “Non-linear Dynamic Analysis of Spur Gear, Analytical and Numerical Studies”, University of Technology, 2005.
• [12] Nahidh M. Ali, “Study of The Response of a Conduit Conveying Fluid Due to a Forced Vibration”, University of Technology, 2011.
• [13] Timoshenko S.P., Young D.H. and Weaver W. Jr., “Vibration Problems in Engineering”, 2nd ed., D. Van Nostrand Company, 2008.

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).